JP2008008154A - Double suction centrifugal pump - Google Patents

Double suction centrifugal pump Download PDF

Info

Publication number
JP2008008154A
JP2008008154A JP2006176570A JP2006176570A JP2008008154A JP 2008008154 A JP2008008154 A JP 2008008154A JP 2006176570 A JP2006176570 A JP 2006176570A JP 2006176570 A JP2006176570 A JP 2006176570A JP 2008008154 A JP2008008154 A JP 2008008154A
Authority
JP
Japan
Prior art keywords
impeller
centrifugal pump
main plate
suction centrifugal
double suction
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2006176570A
Other languages
Japanese (ja)
Other versions
JP2008008154A5 (en
JP4893125B2 (en
Inventor
Takahide Nagahara
孝英 長原
Hideki Akiba
秀樹 秋庭
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Plant Technologies Ltd
Original Assignee
Hitachi Plant Technologies Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Plant Technologies Ltd filed Critical Hitachi Plant Technologies Ltd
Priority to JP2006176570A priority Critical patent/JP4893125B2/en
Publication of JP2008008154A publication Critical patent/JP2008008154A/en
Publication of JP2008008154A5 publication Critical patent/JP2008008154A5/ja
Application granted granted Critical
Publication of JP4893125B2 publication Critical patent/JP4893125B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a double suction centrifugal pump with a good performance not only providing a stable head-capacity curve diagonally right down but also more improving the efficiency of an impeller to largely contribute to reduction of energy consumption. <P>SOLUTION: The invention is characterized in that the double suction centrifugal pump has a pump casing and the impeller rotatably equipped in the pump casing and the impeller has a central main plate, a plurality of symmetrically-shaped blades arranged back to back on opposite surfaces of the main plate and an outer plate provided at ends of the blades which are opposite from the central main plate, wherein the blades are inclined so that the ends on an outer plate side are situated before the ends on a central main plate side in a direction of rotation of the impeller. <P>COPYRIGHT: (C)2008,JPO&INPIT

Description

本発明は遠心ポンプに係わり,特に吸込口を2つ持つ,対称形状の翼を背中合わせに組み合わせた羽根車を用いた両吸込渦巻ポンプの羽根車の改良に係わるものである。   The present invention relates to a centrifugal pump, and more particularly to an improvement of an impeller of a double-suction centrifugal pump using two impellers and an impeller in which symmetrical blades are combined back to back.

主に羽根車の回転による遠心力を流体に与えて昇圧する遠心ポンプにおいて、2つの翼を背中合わせに組み合わせ、一つの吐出しボリュートによって流体を輸送する両吸込渦巻ポンプが知られている。この場合、羽根車の翼は非特許文献1に示されたような対称形状のものを背中合わせに組合わせた形状となっている。 In a centrifugal pump that mainly boosts a fluid by applying centrifugal force generated by rotation of an impeller to the fluid, a double suction centrifugal pump that combines two blades back to back and transports the fluid by one discharge volute is known. In this case, the blades of the impeller have a shape in which symmetrical ones as shown in Non-Patent Document 1 are combined back to back.

ターボポンプ ターボ機械協会編 p168 図11.9Turbo pump Association of turbo machinery p168 Figure 11.9

従来提案されている両吸込渦巻ポンプについて説明する。   A conventionally proposed double suction centrifugal pump will be described.

この両吸込渦巻ポンプは、吸込ケーシング部と吐出ケーシング部からなるポンプケーシングと、対称形状の翼を背中合わせに組み合わせた羽根車によって概略構成されている。   Both the suction centrifugal pumps are roughly constituted by a pump casing composed of a suction casing part and a discharge casing part, and an impeller in which symmetrically shaped blades are combined back to back.

回転軸とともに羽根車が回転することにより両吸込渦巻ポンプ内を流体が移動し、吸込ケーシング部の渦巻形状によって旋回流れが羽根車の吸込口にもたらされる。   When the impeller rotates together with the rotating shaft, the fluid moves in both suction centrifugal pumps, and the swirl flow of the suction casing portion brings the swirling flow to the suction opening of the impeller.

その流体が羽根車に流入した後、羽根車の回転によって流体に遠心力が与えられ、昇圧された後、吐出ケーシング部によって羽根車の吐出口から流出された流体が一つに集められて両吸込渦巻ポンプを出て行くものである。   After the fluid flows into the impeller, centrifugal force is applied to the fluid by the rotation of the impeller, and after the pressure is increased, the fluid that flows out from the discharge port of the impeller is collected together by the discharge casing part. It goes out of the suction centrifugal pump.

この形式の両吸込渦巻ポンプでは、締切付近の低流量域において、入口側に発生する逆流の流れが吸込ケーシングの渦巻形状によって特に抑えられることなく入口付近で旋回する。   In this type of suction pump, the reverse flow generated on the inlet side swirls in the vicinity of the inlet without being particularly suppressed by the spiral shape of the suction casing in the low flow rate region near the deadline.

この旋回する再循環流れによって羽根車の入口付近で角運動量が増加した流れが羽根車に流入するため、全揚程が低下する。この結果として流量―全揚程の性能曲線が右下がりの安定なカーブとならず、締切付近で全揚程が低下して山なりなカーブとなる傾向が強かった。   The swirling recirculation flow causes the flow having an increased angular momentum near the inlet of the impeller to flow into the impeller, so that the total lift is lowered. As a result, there was a strong tendency that the performance curve of the flow-total head did not become a stable curve with a lower right, and the total head was lowered near the deadline, resulting in a mountainous curve.

この場合、例えばポンプの起動時にシステムカーブとの交点が定まらず、運転が不安定になり、最悪の場合はそのままバルブを開放しても規定の流量が出ない場合などが生じ、問題となることが多かった。   In this case, for example, the intersection with the system curve is not determined when the pump is started, and the operation becomes unstable. In the worst case, the specified flow rate does not come out even if the valve is opened as it is. There were many.

本発明の目的は、上記の課題を解決し、右下がりの安定な揚程カーブを提供するのみでなく、羽根車の効率をより一層向上させ、エネルギー消費量の削減に大きく貢献する性能の良い両吸込渦巻ポンプを提供することにある。   The object of the present invention is not only to solve the above-mentioned problems and provide a stable heading curve with a lower right side, but also to improve the efficiency of the impeller further and greatly contribute to the reduction of energy consumption. It is to provide a suction centrifugal pump.

上記目的を解決するために、本発明は、ポンプケーシングと、前記ポンプケーシング内に回転自在に備わる羽根車を有し、前記羽根車は、中央主板と、前記主板の両面に背中合わせに複数配置される対称形状の翼と、前記主板の反対側になる前記翼の端部に設けられる外側板を有する両吸込渦巻ポンプにおいて、前記翼は、前記外側板側の端部が前記中央主板側の端部よりも前記羽根車の回転方向前方に位置するように傾斜していることを特徴とする両吸込み渦巻ポンプにある。   In order to solve the above-mentioned object, the present invention has a pump casing and an impeller rotatably provided in the pump casing, and a plurality of the impellers are arranged back-to-back on both sides of the central main plate and the main plate. A suction vortex pump having a symmetrically shaped wing and an outer plate provided at an end of the wing opposite to the main plate, wherein the wing has an end on the outer plate side on the end of the central main plate side. It is in the double suction centrifugal pump that is inclined so as to be positioned forward of the impeller in the rotational direction of the impeller.

更に具体的には、上記構成の両吸込み渦巻ポンプにおいて、前記中央主板は、前記外側板よりも外径が小さく、前記主板の両面に背中合わせに配置される隣合せの翼が中央主板の外周縁より先側では、中央主板を介さず直に接合することを特徴とする。   More specifically, in the double suction centrifugal pump having the above-described configuration, the central main plate has an outer diameter smaller than that of the outer plate, and adjacent wings arranged back to back on both surfaces of the main plate are outer peripheral edges of the central main plate. The further front side is characterized in that it is joined directly without the central main plate.

また更に具体的には、上記構成の両吸込み渦巻ポンプにおいて、前記主板を挟む一方の翼と他方の翼は、前記羽根車の回転方向にずれていることを特徴とする。   More specifically, in the double suction centrifugal pump configured as described above, one blade and the other blade sandwiching the main plate are shifted in the rotation direction of the impeller.

本発明によれば、右下がりの安定な流量−全揚程カーブが得られ、かつポンプ効率を従来より一層向上させた、性能の良い両吸込渦巻ポンプを提供することができる。   According to the present invention, it is possible to provide a high-performance double-suction centrifugal pump that can obtain a stable flow rate-total head curve that decreases to the right and that has improved the pump efficiency more than before.

本発明の実施例について、図を引用して説明する。   Embodiments of the present invention will be described with reference to the drawings.

以下、本発明の第1の実施例を図1、図3〜図5を参照して説明する。   Hereinafter, a first embodiment of the present invention will be described with reference to FIGS. 1 and 3 to 5.

図1、図3〜図5に示すように、両吸込渦巻ポンプは、羽根車30と、羽根車30を回転自在に内置するポンプケーシング100と、羽根車30を固定する回転軸20を有する。   As shown in FIGS. 1 and 3 to 5, both suction centrifugal pumps have an impeller 30, a pump casing 100 in which the impeller 30 is rotatably installed, and a rotating shaft 20 that fixes the impeller 30.

羽根車30は、図1、図3、図4に示すように、中央主板200と、中央主板200の両面に背中合わせに複数配置される対称形状の翼210と、中央主板200の反対側になる翼210の端部に設けられる外側板220を有する。翼210は、外周側が羽根車30の回転方向後方になる湾曲形状している。   As shown in FIGS. 1, 3, and 4, the impeller 30 is on the opposite side of the central main plate 200, a plurality of symmetrically shaped wings 210 arranged back to back on both sides of the central main plate 200, and the central main plate 200. An outer plate 220 is provided at the end of the wing 210. The blades 210 are curved so that the outer peripheral side is behind the impeller 30 in the rotational direction.

ポンプケーシング100は、図3、図4に示すように、羽根車30の外周吐出側を包むように囲う吐出ケーシング部230と、羽根車30の中心寄り両側に設けられている二つの吸込口240、250に対応する二つの吸込ケーシング部260、270を有する。二つの吸込ケーシング部260、270は渦巻き形状を有する。   As shown in FIGS. 3 and 4, the pump casing 100 includes a discharge casing portion 230 that encloses the outer peripheral discharge side of the impeller 30, and two suction ports 240 provided on both sides near the center of the impeller 30, Two suction casing portions 260 and 270 corresponding to 250 are provided. The two suction casing parts 260 and 270 have a spiral shape.

メカニカルシール280、290は、羽根車30の二つの吸込口240、250と、二つの吸込ケーシング部260、270との摺動部に設けられる。このメカニカルシール280、290により、羽根車3は吐出ケーシング部230側から吸込ケーシング部260、270への流体リークが抑えられる。   The mechanical seals 280 and 290 are provided at sliding portions between the two suction ports 240 and 250 of the impeller 30 and the two suction casing portions 260 and 270. Due to the mechanical seals 280 and 290, the impeller 3 can suppress fluid leakage from the discharge casing portion 230 side to the suction casing portions 260 and 270.

羽根車30の翼210は、図3の(ロ)に示すように、外側板22側の端部が中央主板200側の端部よりも羽根車30の回転方向前方に位置するように傾斜している。   As shown in FIG. 3B, the blades 210 of the impeller 30 are inclined so that the end portion on the outer plate 22 side is located in front of the end portion on the central main plate 200 side in the rotation direction of the impeller 30. ing.

傾斜の角度は、5°〜15°程度の傾きである。また傾斜の角度は、羽根車3の中心側で大きく、外周側で小さい。中心側が10°〜15°、外周側が5°〜10°程度である。   The inclination angle is about 5 ° to 15 °. The angle of inclination is large on the center side of the impeller 3 and small on the outer peripheral side. The central side is about 10 ° to 15 °, and the outer peripheral side is about 5 ° to 10 °.

この翼210の傾斜に関する作用を説明する。   The operation related to the inclination of the blade 210 will be described.

両吸込渦巻ポンプの羽根車内部の流れから説明する。   It demonstrates from the flow inside the impeller of both suction vortex pumps.

一般に両吸込渦巻ポンプに使用される羽根形状は遠心羽根車であり、その内部流れは、非特許文献1「ターボ機械」P35に示されているように非常に複雑である。   Generally, the blade shape used for both suction centrifugal pumps is a centrifugal impeller, and its internal flow is very complicated as shown in Non-Patent Document 1 “Turbomachine” P35.

羽根車の内部流れによって損失がもたらされるメカニズムを概説すると、その大きな要因のひとつに羽根車流路断面方向の面内速度である2次流れの存在があり、これが損失の大小、すなわち羽根車の流線方向の流れの不均一の発生に大きく関わっている。   An outline of the mechanism of loss caused by the internal flow of the impeller is one of the major factors. The existence of the secondary flow, which is the in-plane velocity in the cross-sectional direction of the impeller flow path, is the size of the loss, that is, the flow of the impeller. It is greatly related to the occurrence of non-uniform flow in the linear direction.

図2Aは従来の両吸込渦巻ポンプの羽根車形状を軸方向から見た図、図2Bは従来の羽根車の翼近傍の流れの方向を示す概要図である。   FIG. 2A is a diagram showing the shape of an impeller of a conventional double suction centrifugal pump as viewed from the axial direction, and FIG. 2B is a schematic diagram showing the flow direction in the vicinity of the blades of the conventional impeller.

羽根車内部の主流は,翼の吸込口から翼の吐出口にかけて子午面形状に沿って流れの方向を軸方向から半径方向に変えられる。この際、この主流によってもたらされる遠心力と、子午面でみた中央主板側から外側板側にかけて生じる圧力降下はつりあっているが、翼面付近に生じる境界層内部の流速の遅い部分は遠心力が小さい。   The main flow inside the impeller can be changed from the axial direction to the radial direction along the meridional shape from the suction port of the blade to the discharge port of the blade. At this time, the centrifugal force caused by the main flow and the pressure drop generated from the central main plate side to the outer plate side as seen on the meridian plane are balanced, but the centrifugal force is generated in the part of the boundary layer where the flow velocity is low near the blade surface. small.

このため,圧力勾配に対抗できずに図2Bに示すように中央主板側から外側板側に向かって流れる。   For this reason, it cannot flow against the pressure gradient and flows from the central main plate side toward the outer plate side as shown in FIG. 2B.

更に翼間流路において外側板付近を流れている境界層内の速度の遅い流れも、翼面を沿って流れる主流のコリオリ力によってもたらされる翼圧力面,負圧面間の圧力勾配に対抗できないために、外側板付近を翼圧力面から負圧面方向に流れる。   Furthermore, the slow flow in the boundary layer that flows near the outer plate in the inter-blade flow path cannot counter the pressure gradient between the blade pressure surface and the suction surface caused by the Coriolis force of the mainstream flowing along the blade surface. In addition, it flows in the vicinity of the outer plate from the blade pressure surface toward the suction surface.

従って、それらの主流方向に速度の遅い流れが図2Bに示すように結果的に羽根車の出口付近の翼負圧面、外側板側に集積し、この付近と他の部分で主流方向の速度差が大きくなり、これが翼出口で混合するために損失が生じる。   Therefore, as shown in FIG. 2B, the slow flow in the main flow direction is eventually accumulated on the blade suction surface and the outer plate side near the exit of the impeller, and the speed difference in the main flow direction between this and other portions. Will increase and this will cause loss due to mixing at the blade exit.

従って、この主流方向速度差を抑制して損失を低減するためには、以上説明したような翼流路断面の2次流れをコントロールする必要がある。   Therefore, in order to suppress the main flow direction speed difference and reduce the loss, it is necessary to control the secondary flow in the blade channel cross section as described above.

これに対して、本発明の第1の実施例では、羽根車30が中央主板200と、中央主板の両面に背中合わせに複数配置される対称形状の翼210と、中央主板200の反対側になる翼210の端部に設けられる外側板220を有する両吸込渦巻ポンプにおいて、外側板側220の端部が中央主板200側の端部よりも羽根車30の回転方向前方に位置するように翼210を傾斜させた。   On the other hand, in the first embodiment of the present invention, the impeller 30 is on the opposite side of the central main plate 200, the symmetrically shaped wings 210 that are arranged back to back on both sides of the central main plate, and the central main plate 200. In the double suction centrifugal pump having the outer plate 220 provided at the end of the blade 210, the blade 210 is arranged such that the end of the outer plate 220 is positioned forward of the impeller 30 in the rotation direction with respect to the end of the central main plate 200. Tilted.

この様な形状にすることにより、翼210の吸込口から吐出口にかけて、常に翼の外側板側が回転方向前方に位置して回転することになる。このため、翼210付近の境界層の流れは、図3の(ロ)に示すように、外側板220から中央主板200方向の流れが生じ、これが前述した中央主板200から外側板220にかけて生じている圧力勾配に対抗する。   By adopting such a shape, the outer plate side of the blade is always positioned in front of the rotation direction and rotates from the suction port to the discharge port of the blade 210. For this reason, as shown in FIG. 3B, the boundary layer flow in the vicinity of the wing 210 is generated from the outer plate 220 toward the central main plate 200, and is generated from the central main plate 200 to the outer plate 220 described above. Counters the pressure gradient.

従って、子午面でみた翼210近傍の流れは図2Bの(ロ)に示した従来の羽根と異なり、図3に示すように翼210の出口方向に流れることになる。   Accordingly, the flow in the vicinity of the wing 210 viewed from the meridian plane is different from the conventional blade shown in FIG. 2B (B), and flows in the direction of the exit of the wing 210 as shown in FIG.

この流れの改善によって、翼210の吐出口付近では翼210面付近の境界層内部の速度の遅い流れの集積が弱まり、翼210の吐出口付近において損失を増大させる主流方向速度の不均一を抑制し、羽根車効率が向上する。   By improving the flow, the accumulation of slow flow in the boundary layer near the blade 210 surface near the discharge port of the blade 210 is weakened, and the nonuniformity of the velocity in the main flow direction that increases the loss near the discharge port of the blade 210 is suppressed. As a result, the impeller efficiency is improved.

従ってポンプ効率も向上し、エネルギー消費を抑えた優れた両吸込渦巻ポンプを得ることができる。   Accordingly, the pump efficiency is improved, and an excellent double suction centrifugal pump with reduced energy consumption can be obtained.

以上説明した内容は、ポンプの設計点付近の流れに関するものであるが、次にポンプの締切付近の低流量域における流れの様子について説明する。   The contents described above relate to the flow near the design point of the pump. Next, the state of the flow in the low flow rate region near the pump cutoff will be described.

締切付近では、図4(イ)に示すように、従来の羽根車では吸込口及び吐出口にそれぞれ再循環流れが生じ、羽根車内部の主流は大きく曲げられることになる。   In the vicinity of the deadline, as shown in FIG. 4A, in the conventional impeller, recirculation flows are generated at the suction port and the discharge port, respectively, and the main flow inside the impeller is greatly bent.

特に両吸込渦巻ポンプの場合は吸込ケーシングに渦巻型のものが適用されるため、羽根車の回転とともに回転している吸込口側の再循環流れによって羽根車に流入する流れに大きな旋回が与えられる。吸込口側の角運動量が大きくなり、低流量域では全揚程が低下し、結果として全揚程カーブが山形の特性となる。   In particular, in the case of both suction centrifugal pumps, a spiral type is applied to the suction casing, so that a large swirl is given to the flow flowing into the impeller by the recirculation flow on the suction port side rotating with the rotation of the impeller. . The angular momentum on the suction side increases, and the total lift is lowered in the low flow rate region. As a result, the total lift curve becomes a mountain-shaped characteristic.

これに対して、本発明の第1の実施例では、翼210の吸込口から吐出口にかけて、常に翼210の外側板220側が回転方向前方に位置して回転することで、吐出口の再循環流れの様子が変化する。   In contrast, in the first embodiment of the present invention, the outer plate 220 side of the blade 210 is always positioned forward in the rotation direction from the suction port of the blade 210 to the discharge port, so that the discharge port is recirculated. The flow changes.

すなわち、出口付近での再循環流れは翼流路の相対速度の遅い領域であり、周方向速度が大きくなって遠心力によって昇圧されるため、急激な圧力上昇に耐えきれずに、羽根車30を出た後に再び羽根車30に流れ込むものである。   That is, the recirculation flow in the vicinity of the outlet is a region where the relative speed of the blade flow path is low, and the circumferential speed increases and the pressure is increased by the centrifugal force. After exiting, the air flows into the impeller 30 again.

この流れが本発明の第1実施例の場合は、前述したように速度の遅い境界層内の流れが外側板220から中央主板200方向に流れるために、相対速度の遅い領域が拡大し、図4(ロ)に示すように従来の羽根車と比較して再循環流れの領域が大きくなる。   When this flow is the first embodiment of the present invention, as described above, the flow in the low-speed boundary layer flows from the outer plate 220 toward the central main plate 200, so that the region where the relative velocity is low is enlarged. As shown in FIG. 4 (b), the recirculation flow region becomes larger than that of the conventional impeller.

従って、この逆流域のために翼210の吐出口付近の流出角度が非常に大きくなり、締切付近の低流量域の全揚程を増大させる。   Therefore, because of this reverse flow region, the outflow angle near the discharge port of the blade 210 becomes very large, increasing the total head of the low flow region near the deadline.

その結果、図5に示すように締切から大流量域まで安定した右下がりの全揚程カーブを得られ、運転流量全域において安定したポンプの運転を達成することができる。   As a result, as shown in FIG. 5, a stable right-falling total head curve from the deadline to the large flow rate range can be obtained, and stable pump operation can be achieved over the entire operating flow rate range.

図6は,本発明の第2の実施例に係わる両吸込渦巻ポンプの羽根車30の断面を示すものである。   FIG. 6 shows a cross section of the impeller 30 of the double suction centrifugal pump according to the second embodiment of the present invention.

この実施例でも、羽根車30の外側板220との交線(外側板と翼との交差部)がポンプ回転軸方向から見て中央主板200と翼210の交線よりも回転方向前方に位置していることは実施例1と変わらない。特徴点は、翼210の吐出口付近では中央主板200は存在せず、背中合わせに組み合わされた対称形状の双方の翼210同士で結合している。   Also in this embodiment, the line of intersection with the outer plate 220 of the impeller 30 (the intersection of the outer plate and the blades) is positioned forward in the rotational direction with respect to the line of intersection of the central main plate 200 and the blades 210 when viewed from the pump rotation axis direction. This is the same as in the first embodiment. The feature point is that the central main plate 200 does not exist in the vicinity of the discharge port of the blades 210, and the two blades 210 having symmetrical shapes combined back to back are connected to each other.

すなわち、中央主板200は、外側板220よりも外径が小さく、中央主板200の両面に背中合わせに配置される隣合せの翼210が中央主板200の外周縁より先側では、中央主板200を介さず直に接合する。   That is, the central main plate 200 has an outer diameter smaller than that of the outer plate 220, and the adjacent wings 210 arranged back-to-back on both sides of the central main plate 200 are located on the front side of the outer peripheral edge of the central main plate 200 via the central main plate 200. Connect directly.

この様にすることで,実施例1に示す効果が得られることはもちろん、中央主板200が外周側に存在しないことで摩擦損失も低減でき、更にポンプ効率の良い、エネルギー消費を抑えた両吸込渦巻ポンプを得ることができる。   In this way, the effects shown in the first embodiment can be obtained, and the center main plate 200 is not present on the outer peripheral side, so that friction loss can be reduced, and further high pump efficiency and low energy consumption can be achieved. A vortex pump can be obtained.

図7は、本発明の第3の実施例に係わる両吸込渦巻ポンプの羽根車の断面を示すものである。   FIG. 7 shows a cross section of an impeller of a double suction centrifugal pump according to the third embodiment of the present invention.

この実施例でも、羽根車30の外側板220との交線がポンプ回転軸方向から見て中央主板200と翼210の交線よりも回転方向前方に位置していることは実施例1と変わらない。特徴点は、中央主板200の両面に形成された多数の翼210が羽根車30の回転方向に等ピッチで設けられ、中央主板200の一方に並ぶ翼210と他方に並ぶ翼210が回転方向にずれて背中合わせになっている。   Also in this embodiment, the line of intersection with the outer plate 220 of the impeller 30 is located forward of the rotation direction with respect to the line of intersection of the central main plate 200 and the blades 210 when viewed from the pump rotation axis direction. Absent. A feature point is that a large number of blades 210 formed on both surfaces of the central main plate 200 are provided at an equal pitch in the rotation direction of the impeller 30, and the blades 210 arranged on one side of the central main plate 200 and the blades 210 arranged on the other side in the rotation direction. Misaligned and back to back.

しかも、その回転方向のずれ位置が、中央主板200の反対側に並ぶ翼210間の中間点に来る。   In addition, the rotational position shifts at an intermediate point between the blades 210 arranged on the opposite side of the central main plate 200.

このようにすることで、実施例1に示す効果が得られることはもちろん、羽根車30の翼210から翼210までの流路で生じる回転方向の圧力の変動が、お互いに翼210から翼210までの距離の半分だけ回転方向にずれていることによってお互いに相殺される。   In this way, the effects shown in the first embodiment can be obtained and, of course, fluctuations in the rotational pressure generated in the flow path from the blade 210 to the blade 210 of the impeller 30 are caused by the blade 210 to the blade 210. They are offset from each other by being offset in the direction of rotation by half the distance up to.

このため、羽根車全体として羽根車の吐出口における圧力変動を小さくすることができ,振動や騒音を抑えた両吸込渦巻ポンプを得ることができる。   For this reason, the pressure fluctuation in the discharge port of an impeller can be made small as a whole impeller, and the double suction centrifugal pump which suppressed vibration and noise can be obtained.

本発明の第1の実施例に係わる羽根車の軸方向断面図(ロ)と、羽根車を外周側から見た図(イ)である。They are the axial direction sectional drawing (b) of the impeller concerning the 1st example of the present invention, and the figure (I) which looked at the impeller from the perimeter side. 従来技術の両吸込渦巻ポンプの羽根車形状と内部の流れの様子を示す断面図(ロ)と、羽根車を外周側から見た図(イ)である。It is sectional drawing (B) which shows the state of the impeller shape of the both suction centrifugal pump of a prior art, and the state of an internal flow, and the figure (I) which looked at the impeller from the outer peripheral side. 従来技術の両吸込渦巻ポンプの羽根車の軸方向断面図(ロ)と、羽根車を外周側から見た図(イ)である。They are the axial sectional view (b) of the impeller of the both suction centrifugal pumps of the prior art, and the view (b) of the impeller viewed from the outer peripheral side. 本発明の第1の実施例に係わる両吸込渦巻ポンプの軸方向断面図(イ)と、羽根車内部の流れの様子を示す図(ロ)である。It is an axial sectional view (A) of the both suction centrifugal pump concerning the 1st example of the present invention, and a figure (B) showing a situation of a flow inside an impeller. 本発明の第1の実施例に係わる両吸込渦巻ポンプの羽根車内部の流れの様子を示す断面図(イ)・(ロ)の二例である。It is two examples of sectional drawing (a) and (b) which shows the mode of the flow inside the impeller of the both suction vortex pump concerning the 1st example of the present invention. 本発明の第1の実施例に係わる効果を示す図である。It is a figure which shows the effect concerning the 1st Example of this invention. 本発明の第2の実施例に係わる両吸込渦巻ポンプの断面図(イ)と羽根車の内部の流れの様子を示す図(ロ)である。It is sectional drawing (B) of the both suction vortex pump concerning the 2nd Example of this invention, and the figure (B) which shows the mode of the flow inside an impeller. 本発明の第3の実施例に係わる両吸込渦巻ポンプの断面図(イ)と羽根車の内部の流れの様子を示す図(ロ)である。It is sectional drawing (B) of the both suction vortex pump concerning the 3rd Example of this invention, and the figure (B) which shows the mode of the flow inside an impeller.

符号の説明Explanation of symbols

100…ポンプケーシング、30…羽根車、200…中央主板、210…翼、220…外側板。   DESCRIPTION OF SYMBOLS 100 ... Pump casing, 30 ... Impeller, 200 ... Central main board, 210 ... Wing, 220 ... Outer board.

Claims (9)

ポンプケーシングと、前記ポンプケーシング内に回転自在に備わる羽根車を有し、
前記羽根車は、中央主板と、前記中央主板の両面に背中合わせに複数配置される対称形状の翼と、前記中央主板の反対側になる前記翼の端部に設けられる外側板を有する両吸込渦巻ポンプにおいて、
前記翼は、少なくとも前記羽根車の外周側で、前記外側板側の端部が前記中央主板側の端部よりも前記羽根車の回転方向前方に位置するように傾斜していることを特徴とする両吸込渦巻ポンプ。
A pump casing and an impeller provided rotatably in the pump casing;
The impeller includes a central main plate, a plurality of symmetrically arranged wings arranged back-to-back on both sides of the central main plate, and a double suction vortex having an outer plate provided at an end portion of the wing opposite to the central main plate. In the pump,
The blade is inclined at least on the outer peripheral side of the impeller so that the end on the outer plate side is positioned forward of the end of the impeller in the rotation direction with respect to the end on the central main plate side. Double suction centrifugal pump.
前記請求項1記載の両吸込渦巻ポンプにおいて、
前記中央主板は、前記外側板よりも外径が小さく、
前記主板の両面に背中合わせに配置される隣合せの翼が中央主板の外周縁より先側では、中央主板を介さず直に接合することを特徴とする両吸込み渦巻ポンプ。
The double suction centrifugal pump according to claim 1,
The central main plate has a smaller outer diameter than the outer plate,
A double-suction centrifugal pump characterized in that adjacent wings arranged back-to-back on both surfaces of the main plate are directly joined to each other on the front side of the outer peripheral edge of the central main plate without going through the central main plate.
前記請求項1記載の両吸込渦巻ポンプにおいて、
前記主板を挟む一方の翼と他方の翼は、前記羽根車の回転方向に位置がずれていることを特徴とする両吸込渦巻ポンプ。
The double suction centrifugal pump according to claim 1,
One suction blade and the other blade sandwiching the main plate are misaligned in the rotational direction of the impeller.
前記請求項3記載の両吸込渦巻ポンプにおいて、
前記翼は、前記羽根車の回転方向に等ピッチで設けられ、
前記翼の回転方向のずれ位置が、前記主板の反対側に並ぶ翼間の中間点に来ることを特徴とする両吸込渦巻ポンプ。
In the both suction centrifugal pump according to claim 3,
The blades are provided at an equal pitch in the rotational direction of the impeller,
The double suction centrifugal pump characterized in that the displacement position of the blade in the rotational direction comes to an intermediate point between the blades arranged on the opposite side of the main plate.
前記請求項1記載の両吸込渦巻ポンプにおいて、
前記翼は、外周側が前記羽根車の回転方向後方になる湾曲形状を有することを特徴とする両吸込渦巻ポンプ。
The double suction centrifugal pump according to claim 1,
The double suction pump according to claim 1, wherein the blade has a curved shape in which an outer peripheral side is rearward in the rotation direction of the impeller.
前記請求項1または5記載の両吸込渦巻ポンプにおいて、
前記傾斜は、5°〜15°程度の傾きであることを特徴とする両吸込渦巻ポンプ。
In the double suction centrifugal pump according to claim 1 or 5,
The double suction centrifugal pump characterized in that the inclination is an inclination of about 5 ° to 15 °.
前記請求項1または5記載の両吸込渦巻ポンプにおいて、
前記傾斜の角度は、前記羽根車の中心側で大きく、外周側で小さいことを特徴とする両吸込渦巻ポンプ。
In the double suction centrifugal pump according to claim 1 or 5,
The double suction centrifugal pump characterized in that the angle of inclination is large on the center side of the impeller and small on the outer peripheral side.
前記請求項7記載の両吸込渦巻ポンプにおいて、
前記傾斜の角度は、前記羽根車の中心側が10°〜15°、外周側が5°〜10°程度であることを特徴とする両吸込渦巻ポンプ。
In the double suction centrifugal pump according to claim 7,
The double suction centrifugal pump characterized in that the inclination angle is about 10 ° to 15 ° on the center side of the impeller and about 5 ° to 10 ° on the outer peripheral side.
前記請求項1記載の両吸込渦巻ポンプにおいて、
前記ポンプケーシングは、前記羽根車の外周吐出側を包むように囲う吐出ケーシング部と、前記羽根車の中心寄り両側に設けられている二つの吸込口に対応する二つの吸込ケーシング部とを有し、
前記二つの吸込ケーシング部は渦巻き形状を有することを特徴とする両吸込渦巻ポンプ。
The double suction centrifugal pump according to claim 1,
The pump casing has a discharge casing portion surrounding the outer peripheral discharge side of the impeller, and two suction casing portions corresponding to two suction ports provided on both sides near the center of the impeller,
The two suction centrifugal pumps characterized in that the two suction casing parts have a spiral shape.
JP2006176570A 2006-06-27 2006-06-27 Double suction centrifugal pump Expired - Fee Related JP4893125B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2006176570A JP4893125B2 (en) 2006-06-27 2006-06-27 Double suction centrifugal pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2006176570A JP4893125B2 (en) 2006-06-27 2006-06-27 Double suction centrifugal pump

Publications (3)

Publication Number Publication Date
JP2008008154A true JP2008008154A (en) 2008-01-17
JP2008008154A5 JP2008008154A5 (en) 2009-03-26
JP4893125B2 JP4893125B2 (en) 2012-03-07

Family

ID=39066596

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006176570A Expired - Fee Related JP4893125B2 (en) 2006-06-27 2006-06-27 Double suction centrifugal pump

Country Status (1)

Country Link
JP (1) JP4893125B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109519416A (en) * 2017-09-19 2019-03-26 宁波方太厨具有限公司 A kind of centrifugal blower

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5489601A (en) * 1977-12-27 1979-07-16 Toshiba Corp Guide plate elevating mechanism in recording disc reproducer
JPS5674896A (en) * 1979-11-22 1981-06-20 Toshiba Corp Read only memory element
US4428717A (en) * 1979-10-29 1984-01-31 Rockwell International Corporation Composite centrifugal impeller for slurry pumps
JPS6023300A (en) * 1983-07-16 1985-02-05 極東開発工業株式会社 Automatic stop controller for gondola with winch in height service car
JP2002138991A (en) * 2000-11-06 2002-05-17 Ebara Corp Double suction volute pump

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5489601A (en) * 1977-12-27 1979-07-16 Toshiba Corp Guide plate elevating mechanism in recording disc reproducer
US4428717A (en) * 1979-10-29 1984-01-31 Rockwell International Corporation Composite centrifugal impeller for slurry pumps
JPS5674896A (en) * 1979-11-22 1981-06-20 Toshiba Corp Read only memory element
JPS6023300A (en) * 1983-07-16 1985-02-05 極東開発工業株式会社 Automatic stop controller for gondola with winch in height service car
JP2002138991A (en) * 2000-11-06 2002-05-17 Ebara Corp Double suction volute pump

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109519416A (en) * 2017-09-19 2019-03-26 宁波方太厨具有限公司 A kind of centrifugal blower
CN109519416B (en) * 2017-09-19 2024-01-16 宁波方太厨具有限公司 Centrifugal fan

Also Published As

Publication number Publication date
JP4893125B2 (en) 2012-03-07

Similar Documents

Publication Publication Date Title
JP5316365B2 (en) Turbo fluid machine
JP5495700B2 (en) Centrifugal compressor impeller
JP5221985B2 (en) Centrifugal compressor
JP5233436B2 (en) Centrifugal compressor with vaneless diffuser and vaneless diffuser
CN110230609B (en) Impeller and centrifugal compressor with same
JP6704843B2 (en) Centrifugal compressor and turbocharger
WO2015072231A1 (en) Centrifugal turbomachine
JP5371578B2 (en) Turbine rotor
JP4924984B2 (en) Cascade of axial compressor
WO2011007466A1 (en) Impeller and rotary machine
RU2568355C2 (en) Compressor and gas-turbine engine with optimised efficiency
JP6126743B2 (en) Propeller pump for pumping liquid
JP2009133267A (en) Impeller of compressor
JP2006002689A (en) Fan
JP2008208753A (en) Centrifugal compressor
JP5558183B2 (en) Turbo machine
US11572890B2 (en) Blade and axial flow impeller using same
JP4893125B2 (en) Double suction centrifugal pump
JP4696774B2 (en) Double suction centrifugal pump
JP6785623B2 (en) Fluid machine
JP4655603B2 (en) Centrifugal compressor
JP4174693B2 (en) Centrifugal compressor diffuser
JP2010190221A (en) Blower
JP2005054717A (en) Blower impeller
EP3530957B1 (en) Compressor and turbocharger

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20090204

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20090204

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20110601

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20110607

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20110803

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20110830

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20111031

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20111122

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20111205

R150 Certificate of patent or registration of utility model

Ref document number: 4893125

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20150106

Year of fee payment: 3

S111 Request for change of ownership or part of ownership

Free format text: JAPANESE INTERMEDIATE CODE: R313111

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

S111 Request for change of ownership or part of ownership

Free format text: JAPANESE INTERMEDIATE CODE: R313111

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

LAPS Cancellation because of no payment of annual fees